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MH 108 11.98% (mh108-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 108 11.98% (mh108-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.05 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh108-il-1000000.txt
Download as CSV file: xf-mh108-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 108  11.98%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.8010   0.15437   0.15261   0.0386   1.0000   0.0042
 -16.250  -0.8715   0.13014   0.12811   0.0257   1.0000   0.0039
 -16.000  -0.9027   0.11784   0.11568   0.0188   1.0000   0.0038
 -15.750  -0.9354   0.10601   0.10370   0.0121   1.0000   0.0037
 -15.500  -0.9638   0.09585   0.09339   0.0062   1.0000   0.0036
 -15.250  -0.9889   0.08678   0.08421   0.0010   1.0000   0.0036
 -15.000  -1.0180   0.07719   0.07447  -0.0047   1.0000   0.0035
 -14.750  -1.0451   0.06814   0.06526  -0.0101   1.0000   0.0035
 -14.500  -1.0692   0.05975   0.05671  -0.0155   1.0000   0.0035
 -14.250  -1.0882   0.05247   0.04927  -0.0203   1.0000   0.0035
 -14.000  -1.1020   0.04655   0.04319  -0.0241   1.0000   0.0034
 -13.750  -1.1153   0.04152   0.03799  -0.0268   1.0000   0.0034
 -13.500  -1.1255   0.03769   0.03402  -0.0279   1.0000   0.0035
 -13.250  -1.1344   0.03463   0.03083  -0.0277   1.0000   0.0035
 -13.000  -1.1404   0.03226   0.02831  -0.0263   1.0000   0.0035
 -12.750  -1.1454   0.03027   0.02619  -0.0241   1.0000   0.0035
 -12.500  -1.1474   0.02867   0.02449  -0.0214   1.0000   0.0035
 -12.250  -1.1485   0.02724   0.02293  -0.0181   1.0000   0.0035
 -12.000  -1.1468   0.02602   0.02160  -0.0148   1.0000   0.0036
 -11.750  -1.1391   0.02482   0.02030  -0.0123   1.0000   0.0037
 -11.500  -1.1281   0.02367   0.01904  -0.0103   1.0000   0.0037
 -11.250  -1.1150   0.02260   0.01787  -0.0084   1.0000   0.0037
 -11.000  -1.1000   0.02161   0.01678  -0.0067   1.0000   0.0039
 -10.750  -1.0842   0.02062   0.01569  -0.0051   1.0000   0.0039
 -10.500  -1.0666   0.01974   0.01471  -0.0036   1.0000   0.0040
 -10.250  -1.0481   0.01890   0.01379  -0.0023   1.0000   0.0041
 -10.000  -1.0283   0.01817   0.01298  -0.0011   1.0000   0.0044
  -9.750  -1.0082   0.01742   0.01216   0.0001   1.0000   0.0044
  -9.500  -0.9862   0.01686   0.01153   0.0011   1.0000   0.0046
  -9.250  -0.9679   0.01584   0.01040   0.0026   1.0000   0.0049
  -9.000  -0.9476   0.01504   0.00953   0.0038   1.0000   0.0053
  -8.750  -0.9251   0.01447   0.00891   0.0048   1.0000   0.0056
  -8.500  -0.9019   0.01398   0.00837   0.0056   1.0000   0.0059
  -8.250  -0.8785   0.01350   0.00785   0.0065   1.0000   0.0063
  -8.000  -0.8546   0.01309   0.00740   0.0073   1.0000   0.0067
  -7.750  -0.8324   0.01245   0.00670   0.0084   1.0000   0.0077
  -7.500  -0.8088   0.01201   0.00624   0.0092   1.0000   0.0089
  -7.250  -0.7856   0.01153   0.00574   0.0102   1.0000   0.0111
  -7.000  -0.7627   0.01104   0.00527   0.0112   1.0000   0.0161
  -6.750  -0.7397   0.01061   0.00489   0.0122   1.0000   0.0236
  -6.500  -0.7168   0.01021   0.00456   0.0133   1.0000   0.0326
  -6.250  -0.6793   0.00977   0.00422   0.0111   0.9840   0.0455
  -6.000  -0.6352   0.00942   0.00389   0.0076   0.9259   0.0596
  -5.750  -0.6125   0.00931   0.00363   0.0090   0.8598   0.0708
  -5.500  -0.5888   0.00918   0.00340   0.0100   0.8170   0.0834
  -5.250  -0.5641   0.00902   0.00319   0.0108   0.7817   0.0973
  -5.000  -0.5388   0.00886   0.00298   0.0114   0.7507   0.1128
  -4.750  -0.5133   0.00867   0.00278   0.0120   0.7234   0.1317
  -4.500  -0.4874   0.00850   0.00260   0.0124   0.6995   0.1500
  -4.250  -0.4612   0.00835   0.00243   0.0129   0.6762   0.1676
  -4.000  -0.4347   0.00823   0.00228   0.0133   0.6537   0.1847
  -3.750  -0.4084   0.00807   0.00213   0.0137   0.6327   0.2058
  -3.250  -0.3552   0.00779   0.00187   0.0144   0.5958   0.2501
  -3.000  -0.3285   0.00766   0.00176   0.0147   0.5778   0.2744
  -2.750  -0.3018   0.00753   0.00165   0.0150   0.5602   0.3007
  -2.500  -0.2751   0.00740   0.00156   0.0154   0.5434   0.3288
  -2.250  -0.2484   0.00728   0.00148   0.0157   0.5280   0.3580
  -2.000  -0.2215   0.00717   0.00140   0.0160   0.5133   0.3858
  -1.750  -0.1948   0.00705   0.00134   0.0163   0.4988   0.4190
  -1.500  -0.1682   0.00693   0.00128   0.0167   0.4845   0.4526
  -1.250  -0.1415   0.00682   0.00123   0.0170   0.4705   0.4861
  -1.000  -0.1149   0.00672   0.00119   0.0174   0.4578   0.5212
  -0.750  -0.0886   0.00660   0.00116   0.0178   0.4457   0.5610
  -0.500  -0.0625   0.00648   0.00113   0.0183   0.4340   0.6038
  -0.250  -0.0366   0.00637   0.00112   0.0188   0.4222   0.6469
   0.000  -0.0108   0.00626   0.00111   0.0194   0.4109   0.6900
   0.250   0.0148   0.00616   0.00112   0.0200   0.4005   0.7335
   0.500   0.0402   0.00608   0.00114   0.0208   0.3907   0.7752
   0.750   0.0659   0.00600   0.00116   0.0215   0.3814   0.8141
   1.000   0.0919   0.00596   0.00121   0.0221   0.3725   0.8507
   1.250   0.1188   0.00596   0.00126   0.0226   0.3632   0.8831
   1.500   0.1477   0.00597   0.00133   0.0227   0.3554   0.9109
   1.750   0.1801   0.00607   0.00142   0.0219   0.3468   0.9312
   2.000   0.2145   0.00617   0.00151   0.0208   0.3390   0.9454
   2.250   0.2473   0.00631   0.00161   0.0199   0.3314   0.9562
   2.500   0.2819   0.00643   0.00171   0.0186   0.3245   0.9634
   2.750   0.3139   0.00658   0.00181   0.0179   0.3175   0.9699
   3.000   0.3521   0.00669   0.00190   0.0158   0.3113   0.9726
   3.250   0.3880   0.00685   0.00201   0.0142   0.3044   0.9762
   3.500   0.4183   0.00696   0.00212   0.0139   0.2994   0.9817
   3.750   0.4569   0.00707   0.00220   0.0116   0.2932   0.9833
   4.000   0.4944   0.00719   0.00230   0.0096   0.2874   0.9852
   4.250   0.5312   0.00728   0.00238   0.0077   0.2818   0.9874
   4.500   0.5665   0.00742   0.00249   0.0062   0.2754   0.9901
   4.750   0.6008   0.00751   0.00259   0.0049   0.2706   0.9928
   5.000   0.6367   0.00761   0.00267   0.0032   0.2643   0.9945
   5.250   0.6738   0.00771   0.00276   0.0012   0.2584   0.9963
   5.500   0.7119   0.00778   0.00283  -0.0010   0.2516   0.9984
   5.750   0.7478   0.00790   0.00294  -0.0028   0.2449   1.0000
   6.000   0.7723   0.00797   0.00303  -0.0021   0.2389   1.0000
   6.250   0.7963   0.00813   0.00316  -0.0014   0.2314   1.0000
   6.500   0.8208   0.00822   0.00328  -0.0007   0.2251   1.0000
   6.750   0.8448   0.00839   0.00342   0.0001   0.2161   1.0000
   7.000   0.8689   0.00856   0.00357   0.0008   0.2063   1.0000
   7.250   0.8929   0.00875   0.00376   0.0015   0.1961   1.0000
   7.500   0.9165   0.00899   0.00396   0.0023   0.1844   1.0000
   7.750   0.9396   0.00928   0.00420   0.0031   0.1697   1.0000
   8.000   0.9624   0.00960   0.00447   0.0039   0.1560   1.0000
   8.250   0.9853   0.00992   0.00476   0.0048   0.1448   1.0000
   8.500   1.0077   0.01028   0.00508   0.0056   0.1330   1.0000
   8.750   1.0298   0.01068   0.00543   0.0065   0.1202   1.0000
   9.000   1.0515   0.01110   0.00579   0.0075   0.1077   1.0000
   9.250   1.0731   0.01153   0.00618   0.0085   0.0963   1.0000
   9.500   1.0940   0.01201   0.00660   0.0095   0.0839   1.0000
   9.750   1.1148   0.01249   0.00704   0.0105   0.0732   1.0000
  10.000   1.1351   0.01300   0.00751   0.0116   0.0626   1.0000
  10.250   1.1554   0.01350   0.00799   0.0127   0.0543   1.0000
  10.500   1.1747   0.01407   0.00852   0.0139   0.0458   1.0000
  10.750   1.1931   0.01470   0.00912   0.0152   0.0379   1.0000
  11.000   1.2116   0.01530   0.00971   0.0165   0.0320   1.0000
  11.250   1.2293   0.01595   0.01034   0.0178   0.0261   1.0000
  11.500   1.2459   0.01665   0.01105   0.0192   0.0215   1.0000
  11.750   1.2617   0.01738   0.01178   0.0207   0.0178   1.0000
  12.000   1.2771   0.01810   0.01253   0.0223   0.0146   1.0000
  12.250   1.2902   0.01893   0.01338   0.0240   0.0117   1.0000
  12.500   1.3017   0.01982   0.01429   0.0259   0.0096   1.0000
  12.750   1.3116   0.02073   0.01525   0.0279   0.0079   1.0000
  13.000   1.3169   0.02169   0.01626   0.0306   0.0071   1.0000
  13.250   1.3127   0.02297   0.01762   0.0342   0.0061   1.0000
  13.500   1.3159   0.02422   0.01895   0.0359   0.0056   1.0000
  13.750   1.3169   0.02600   0.02082   0.0367   0.0053   1.0000
  14.000   1.3136   0.02870   0.02363   0.0365   0.0047   1.0000
  14.250   1.3028   0.03283   0.02790   0.0348   0.0043   1.0000
  14.500   1.3016   0.03609   0.03128   0.0334   0.0041   1.0000
  14.750   1.2976   0.03981   0.03511   0.0317   0.0040   1.0000
  15.000   1.2865   0.04449   0.03991   0.0295   0.0042   1.0000
  15.250   1.2793   0.04864   0.04417   0.0277   0.0039   1.0000
  15.500   1.2645   0.05382   0.04947   0.0254   0.0039   1.0000
  15.750   1.2531   0.05855   0.05429   0.0235   0.0036   1.0000
  16.000   1.2339   0.06439   0.06025   0.0210   0.0035   1.0000
  16.250   1.2166   0.07003   0.06600   0.0186   0.0036   1.0000
  16.500   1.2021   0.07551   0.07158   0.0162   0.0036   1.0000
  16.750   1.1849   0.08152   0.07769   0.0135   0.0035   1.0000
  17.000   1.1718   0.08701   0.08328   0.0111   0.0037   1.0000
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